Notes on Numerical Fluid Mechanics (NNFM) - Computation and Comparison of Efficient Turbulence Models for Aeronautics — European Research Project ETMA
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9783322898616, 9783322898593

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Unsteady Separated Turbulent Flows Computation with Wall-Laws and k — ε Model

Notes on Numerical Fluid Mechanics (NNFM) - Computation and Comparison of Efficient Turbulence Models for Aeronautics — European Research Project ETMA ◽

10.1007/978-3-322-89859-3_60 ◽

1998 ◽

pp. 549-560

Author(s):

Bijan Mohammadi

Keyword(s):

Turbulent Flows

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Presentation of TC8: Flow around airfoil (steady)

Notes on Numerical Fluid Mechanics (NNFM) - Computation and Comparison of Efficient Turbulence Models for Aeronautics — European Research Project ETMA ◽

10.1007/978-3-322-89859-3_50 ◽

1998 ◽

pp. 475-478

Author(s):

Leslie J. Johnston

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Numerical simulation of supersonic mixing layers at different convective Mach numbers with a k — ε model

Notes on Numerical Fluid Mechanics (NNFM) - Computation and Comparison of Efficient Turbulence Models for Aeronautics — European Research Project ETMA ◽

10.1007/978-3-322-89859-3_5 ◽

1998 ◽

pp. 37-44

Author(s):

C. Le Ribault

Keyword(s):

Numerical Simulation ◽

Mixing Layers ◽

Supersonic Mixing ◽

Mach Numbers ◽

Supersonic Mixing Layers

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Computations on the Compression Ramp Using Explicit Algebraic Reynolds Stress Models

Notes on Numerical Fluid Mechanics (NNFM) - Computation and Comparison of Efficient Turbulence Models for Aeronautics — European Research Project ETMA ◽

10.1007/978-3-322-89859-3_38 ◽

1998 ◽

pp. 350-363

Author(s):

Stefan Wallin

Keyword(s):

Reynolds Stress ◽

Compression Ramp ◽

Stress Models

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Computation of a shock wave boundary layer interaction on compression ramp flow configuration

Notes on Numerical Fluid Mechanics (NNFM) - Computation and Comparison of Efficient Turbulence Models for Aeronautics — European Research Project ETMA ◽

10.1007/978-3-322-89859-3_36 ◽

1998 ◽

pp. 331-335

Author(s):

H. Loyau ◽

D. Vandromme

Keyword(s):

Boundary Layer ◽

Shock Wave ◽

Flow Configuration ◽

Layer Interaction ◽

Wave Boundary Layer ◽

Boundary Layer Interaction ◽

Compression Ramp ◽

Wave Boundary

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Study of the Supersonic Compression Ramp Flow Using the k-ε Turbulence Model with and Without Algebraic Reynolds Stress Modifications

Notes on Numerical Fluid Mechanics (NNFM) - Computation and Comparison of Efficient Turbulence Models for Aeronautics — European Research Project ETMA ◽

10.1007/978-3-322-89859-3_34 ◽

1998 ◽

pp. 311-322

Author(s):

C. Vassilopoulos ◽

K. C. Giannakoglou ◽

K. D. Papailiou

Keyword(s):

Reynolds Stress ◽

Turbulence Model ◽

Compression Ramp

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Solutions of Non-Equilibrium Wall Boundary Layers with a Low-Re-Number Second Moment Closure

Notes on Numerical Fluid Mechanics (NNFM) - Computation and Comparison of Efficient Turbulence Models for Aeronautics — European Research Project ETMA ◽

10.1007/978-3-322-89859-3_26 ◽

1998 ◽

pp. 231-240

Author(s):

S. Jakirlić ◽

K. Hanjalić ◽

I. Hadžić

Keyword(s):

Boundary Layers ◽

Moment Closure ◽

Second Moment ◽

Wall Boundary ◽

Second Moment Closure ◽

Non Equilibrium

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Incompressible Recirculating Flows

Notes on Numerical Fluid Mechanics (NNFM) - Computation and Comparison of Efficient Turbulence Models for Aeronautics — European Research Project ETMA ◽

10.1007/978-3-322-89859-3_14 ◽

1998 ◽

pp. 111-118

Author(s):

Robert D. Harper ◽

Michael M. Gibson

Keyword(s):

Recirculating Flows

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Computational Results on Test Cases TC-2C and TC2-D Two Dimensional, Incompressible Flows with Recirculation

Notes on Numerical Fluid Mechanics (NNFM) - Computation and Comparison of Efficient Turbulence Models for Aeronautics — European Research Project ETMA ◽

10.1007/978-3-322-89859-3_13 ◽

1998 ◽

pp. 103-110

Author(s):

J. J. Schmidt ◽

P. S. Larsen

Keyword(s):

Incompressible Flows ◽

Test Cases ◽

Computational Results ◽

Two Dimensional

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Flat Plate Boundary Layers

Notes on Numerical Fluid Mechanics (NNFM) - Computation and Comparison of Efficient Turbulence Models for Aeronautics — European Research Project ETMA ◽

10.1007/978-3-322-89859-3_21 ◽

1998 ◽

pp. 190-197

Author(s):

Adil A. Dafa’Alla ◽

Robert D. Harper ◽

Michael M. Gibson

Keyword(s):

Flat Plate ◽

Boundary Layers ◽

Plate Boundary

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Notes on Numerical Fluid Mechanics (NNFM) - Computation and Comparison of Efficient Turbulence Models for Aeronautics — European Research Project ETMALatest Publications

TOTAL DOCUMENTS

H-INDEX

Published By Vieweg+Teubner Verlag

Unsteady Separated Turbulent Flows Computation with Wall-Laws and k — ε Model

Presentation of TC8: Flow around airfoil (steady)

Numerical simulation of supersonic mixing layers at different convective Mach numbers with a k — ε model

Computations on the Compression Ramp Using Explicit Algebraic Reynolds Stress Models

Computation of a shock wave boundary layer interaction on compression ramp flow configuration

Study of the Supersonic Compression Ramp Flow Using the k-ε Turbulence Model with and Without Algebraic Reynolds Stress Modifications

Solutions of Non-Equilibrium Wall Boundary Layers with a Low-Re-Number Second Moment Closure

Incompressible Recirculating Flows

Computational Results on Test Cases TC-2C and TC2-D Two Dimensional, Incompressible Flows with Recirculation

Flat Plate Boundary Layers

Notes on Numerical Fluid Mechanics (NNFM) - Computation and Comparison of Efficient Turbulence Models for Aeronautics — European Research Project ETMA
Latest Publications